EP2636890B1 - Anordnung zum Verstellen des Anstellwinkels eines Rotorblatts - Google Patents

Anordnung zum Verstellen des Anstellwinkels eines Rotorblatts Download PDF

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Publication number
EP2636890B1
EP2636890B1 EP12158855.2A EP12158855A EP2636890B1 EP 2636890 B1 EP2636890 B1 EP 2636890B1 EP 12158855 A EP12158855 A EP 12158855A EP 2636890 B1 EP2636890 B1 EP 2636890B1
Authority
EP
European Patent Office
Prior art keywords
blade
tip
rotor
rotor blade
blade part
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP12158855.2A
Other languages
English (en)
French (fr)
Other versions
EP2636890A1 (de
Inventor
Jason Stege
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Priority to EP12158855.2A priority Critical patent/EP2636890B1/de
Priority to DK12158855.2T priority patent/DK2636890T3/en
Priority to US13/783,709 priority patent/US20130236307A1/en
Publication of EP2636890A1 publication Critical patent/EP2636890A1/de
Application granted granted Critical
Publication of EP2636890B1 publication Critical patent/EP2636890B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06—Rotors
    • F03D1/065—Rotors characterised by their construction elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022—Adjusting aerodynamic properties of the blades
    • F03D7/0224—Adjusting blade pitch
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06—Rotors
    • F03D1/065—Rotors characterised by their construction elements
    • F03D1/0658—Arrangements for fixing wind-engaging parts to a hub
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022—Adjusting aerodynamic properties of the blades
    • F03D7/0224—Adjusting blade pitch
    • F03D7/0228—Adjusting blade pitch of the blade tips only
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • F03D80/30—Lightning protection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/302—Segmented or sectional blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/50—Bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/50—Bearings
    • F05B2240/53—Hydrodynamic or hydrostatic bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00—Control
    • F05B2270/60—Control system actuates through
    • F05B2270/605—Control system actuates through pneumatic actuators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Definitions

  • the invention describes a rotor blade pitching arrangement, a two-part wind turbine rotor blade, a wind turbine, and a method of adjusting a pitching angle of a two-part wind turbine rotor blade.
  • the pitching angle of a rotor blade is usually set by a pitch bearing arranged between a root of the rotor blade and the hub of the wind turbine.
  • the pitch bearing is used to rotate the rotor blade about an axis of rotation relative to the hub.
  • the blade root and the pitch bearing are circular, so that pitch bearing can effectively rotate the blade about an axis of rotation essentially perpendicular to-the hub.
  • pitch bearing can effectively rotate the blade about an axis of rotation essentially perpendicular to-the hub.
  • the ability of the wind turbine to extract energy from the air depends on the shape of the rotor blade, and a prior art rotor blade therefore generally comprises an airfoil shape over a significant portion of its length, starting at a "shoulder" or transition region between the necessarily circular pitch bearing end of the blade, where the airfoil shape is widest, and extending some or most of the way to the outer or tip end of the blade.
  • Such an airfoil shape requires usually quite cost-intensive manufacturing techniques such as dedicated moulds for moulding a composite blade in the desired shape.
  • a longer blade generally implies increased surface area, increased volume and increased mass, and therefore also increased manufacturing costs.
  • the generally hollow rotor blades require complex moulding processes to obtain a desired long but stable blade.
  • a pitch system for such a long blade must also be equipped with a more powerful motor or other actuator to rotate the heavy rotor blade about its axis.
  • Such pitch systems represent a considerable part of the overall cost of a wind turbine.
  • a longer blade, with a correspondingly longer airfoil section will also be subject to more loading along its length, and the increased loading may result in material failure of the blade or damage to the bearings.
  • the rotor blade pitching arrangement for a two-part wind turbine rotor blade comprises a fluid bearing realised to connect a tip blade part to a main blade part such that the tip blade part is rotatable relative to the main blade part about an axis of rotation; and a pitch angle adjusting means for obtaining a specific pitching angle for the tip blade part to increase and decrease a rotational speed of a rotor of the wind turbine.
  • main blade part and tip blade part are to be understood as “inner” and “outer” blade parts respectively, i.e. the main blade part is mounted or connected to a hub of the wind turbine and comprises an inner portion of the rotor blade, while the tip blade part comprises an outer portion of the rotor blade.
  • An advantage of the rotor blade pitching arrangement according to the invention is that an adjustment of a pitching angle of only the tip blade part can suffice to increase or decrease the rotor speed during normal operation of the wind turbine.
  • Such a wind turbine design can therefore dispense with an airfoil shape over the main blade part. Since it may be sufficient that only the tip blade part is given a significant airfoil shape for converting kinetic energy of the wind into rotational energy of the wind turbine rotor, such a blade design can be very economical to realise.
  • Another advantage of the rotor blade pitching arrangement according to the invention is that a rotation of the tip blade part relative to the main blade part can be obtained with a favourably low effort, since a fluid bearing between the outer tip blade part and the main blade part can be realised to have very low or even negligible friction between any bearing surfaces, since such a fluid bearing is not subject to the high loads acting on a bearing of a prior art pitching system between a hub and an entire prior art blade as described in the introduction.
  • the two-part wind turbine rotor blade comprises a tip blade part, a main blade part and a fluid bearing realised to connect the tip blade part to the main blade part such that the tip blade part is rotatable relative to the main blade part about an axis of rotation; wherein the fluid bearing is realised for connection to a pitch angle adjusting means for obtaining a specific pitching angle of the tip blade part relative to the main blade part to increase and decrease a rotational speed of a rotor of the wind turbine.
  • An advantage of the rotor blade according to the invention is that it can be manufactured in a significantly more economical manner. Since a pitching of the tip blade section can suffice to control the rotational speed of the rotor, it may be sufficient to only provide this part of the two-part blade with a significant airfoil shape.
  • the main part of the blade can have a simpler shape, can be considerably more economical to manufacture, and can also be significantly less massive than a prior art wind turbine rotor blade. Accordingly, such a two-part rotor blade according to the invention can be significantly lighter or less massive than a prior art rotor blade of the same length. Equally, a two-part rotor blade according to the invention can be significantly longer than a prior art rotor blade of the same mass, so that a wind turbine equipped with such longer blades can be more efficient and can generate more output power.
  • a fluid bearing for such a rotor blade pitching arrangement of such a two-part wind turbine rotor blade preferably comprises a moveable bearing part realised to be actuated by a pitch angle adjusting means of the rotor blade pitching arrangement such that a motion of the bearing part results in a corresponding rotation of the tip blade part relative to the main blade part about an axis of rotation to obtain a specific pitching angle of the tip blade part.
  • a significant advantage of such a fluid bearing is that, compared to other bearings such as ball bearings or needle bearings that require precisely machined parts and are therefore comparatively expensive, a fluid bearing is quite easy to manufacture at relatively low cost, and exhibits a very low degree of friction. Therefore, very little physical effort is required to actuate the moveable part of the bearing.
  • the fluid bearing can be connected or mounted in any suitable manner to the tip blade part such that a movement of the bearing part of the fluid bearing results in a corresponding rotation of the tip blade part, since the tip blade part is rotatably arranged relative to the main blade part.
  • the fluid bearing can be arranged partially or wholly within the tip blade part.
  • the wind turbine comprises a number of such two-part wind turbine rotor blades arranged to rotate a rotor of the wind turbine, and wherein the speed of the rotor is increased and decreased according to a pitching angle of a tip blade part of a two-part rotor blade, also during normal operation of the wind turbine, and wherein the pitching angle of a tip blade part of a two-part rotor blade is controlled by a rotor blade pitching arrangement according to the invention.
  • An advantage of the wind turbine according to the invention is that, for the reasons given above, the efficiency and power output of the wind turbine can be significantly increased compared to wind turbines with prior art rotor blades of the same length or of the same mass as the two-part rotor blades. In a wind park comprising a multitude of such wind turbines, the overall power output can be significantly increased. Furthermore, the costs of manufacturing such a wind turbine can be reduced, since the two-part blades can be manufactured using less material and with less effort.
  • the method of adjusting a pitch angle of a two-part wind turbine rotor blade of a wind turbine comprises the steps of determining a desired pitching angle for the tip blade part of a two-part rotor blade; determining an extent of motion of a moveable bearing part of the fluid bearing of the two-part blade to achieve that pitching angle; and controlling a pitch angle adjusting means of the rotor blade pitching arrangement accordingly.
  • An advantage of the method according to the invention is that a very precise control of the rotor speed of the wind turbine is possible. This is because the pitching angle of the outer part of the blade - i.e. the tip blade part - need only be slightly adjusted in order to obtain a significant increase in rotor speed, depending on the momentary requirements, or a decrease in rotor speed, if this is desired. A change in pitching angle at the outer region of a blade is more effective than changing the pitching angle of a lower region of the blade, as is known from the pitching systems of the prior art mentioned in the introduction.
  • the terms “two-part blade” and “split blade” may be used interchangeably, in the following, and the terms “blade section” and “blade part” may be used interchangeably also.
  • a blade part can comprise several parts joined together to act as a single blade part.
  • the overall length of the split blade essentially comprises the combined lengths of the main blade part and the tip blade part. It may be assumed in the following - again without restricting the invention in any way - that the main blade part comprises a significantly greater mass than the tip blade part, and/or that the main blade part is significantly longer than the tip blade part.
  • the length of the main blade part comprises at least 60%, more preferably at least 75%, most preferably at least 90% of the overall blade length, and the remaining portion of the overall blade length is given in each case by the tip blade part.
  • specific pitching angle can be understood to mean a specific angle relative to a known reference, for example relative to a known reference position of the tip blade part relative to the main blade part.
  • specific pitching angle can mean an angle with a measure of tolerance either side, for example ⁇ 0.5°, ⁇ 0.1°, etc., so that an acceptable degree of precision is obtained.
  • specific pitching angle can also be understood to mean an angle that results in a desired rotational speed of a rotor of wind turbine generator. In this case the moveable bearing part can be repeatedly or continuously actuated by the pitch angle adjusting means until the desired rotational speed is obtained.
  • the extent of rotation of the tip blade part relative to the main blade part can be controlled in both directions, i.e. into the wind and out of the wind.
  • Any suitable kind of fluid bearing can be implemented to allow the tip blade part to rotate about an axis of rotation relative to the main blade part.
  • the pitch angle adjusting means preferably comprises a fluid source for injecting a controlled volume of a pressurized fluid into the fluid bearing such that the tip blade part rotates relative to the main blade part, wherein a fluid volume is directly related to a pitching angle of the tip blade part relative to the main blade part.
  • the fluid source of the rotor blade pitching arrangement can be controlled to force a fluid into the fluid bearing, such that the tip blade part is pitched into the wind.
  • the fluid source can be controlled to reduce or halt a flow of pressurized fluid into the fluid bearing.
  • the fluid bearing is a hydrostatic bearing.
  • a fluid such as a suitable oil could be used to keep the bearing surfaces, or bearing pads, separate and to allow the tip section to rotate relative to the main blade section.
  • the fluid source comprises a source of pressurized air
  • the fluid bearing comprises an aerostatic bearing.
  • a bearing pad of such a fluid bearing is preferably made of polymer, or at least comprises a polymer layer on its inner surface, i.e. the surface facing into a cavity or air space between bearing surfaces.
  • the fluid bearing comprises a pair of bearing pads with opposing bearing faces, arranged between the main blade part and the tip blade part, such that one bearing pad is oriented towards the inner end of the rotor blade and the other bearing pad is oriented toward the outer end of the rotor blade.
  • the fluid bearing can be realised such that both bearing pads are moveable, or such that one bearing pad remains stationary relative to the rotor blade while the other bearing pad can be moved in an "inward” or “outward” direction, for example toward or away from the stationary bearing pad.
  • the "inner” bearing pad is stationary, while the “outer” bearing pad is moveable relative to the inner pad.
  • a centrifugal force acts in a radially outward direction on the tip blade part.
  • the rotor blade pitching arrangement makes use of this fact to efficiently control the pitching angle of the tip blade section, and the pitch angle adjusting means is realised to inject or force compressed or pressurized air into the fluid bearing in a direction essentially opposite to the direction of the centrifugal force acting on the tip blade part.
  • the centrifugal force effectively assists the procedure, since it helps to "push" the moveable bearing pad in a radially outward direction.
  • the compressed-air source can be realised to release controlled amounts of pressurized air into the bearing, and can equally be realized to intake air from the bearing.
  • the compressed-air source can comprise one or more valves arranged appropriately.
  • the rotor blade pitching arrangement is preferably realised such that by injecting a controlled volume or controlled amount of pressurized air into the fluid bearing, the tip blade section is pitched into the wind.
  • the pitch angle adjusting means can be realised to remove a volume of air from between the bearing pads in order to pitch the tip blade section out of the wind.
  • a "controlled volume" of pressurized air can be released from the compressed air source or from the fluid bearing by, for example, opening a valve for a predetermined duration of time or until a pressure-sensing means such as a manometer indicates that the controlled volume has been released, etc.
  • the rotor blade pitching arrangement comprises a wind sensor arranged to detect a wind condition, and preferably connected to the compressed-air source so that this can respond accordingly.
  • the rotor blade pitching arrangement can receive an input from, for example, a plant controller of the wind park, specifying that the rotor rotational speed should be adjusted to regulate the power.output of the wind turbine.
  • the rotor blade pitching arrangement comprises a control unit for controlling the fluid source on the basis of a sensor output to achieve a desired pitching angle.
  • This control unit can be realised as, for example, a micro-controller connected to the sensor output and arranged in the tip blade section.
  • the control unit can be located at any suitable part of the wind turbine.
  • the fluid bearing can be realised to respond in a controlled manner to the pressure of the fluid being forced into it.
  • an increase in air pressure by a certain amount can be associated with an increase of the pitch angle by a corresponding fraction of a degree.
  • increasing the air pressure by a certain amount would result in a certain increase in pitch angle. Accordingly, allowing the air pressure to drop by the same amount would result in the tip blade section being pitched out of the wind by that amount.
  • the compressed-air source can be "informed" of the momentary pitch angle, and can increase or decrease the air pressure to alter the pitch angle as required.
  • the rotor blade pitching arrangement comprises a pitching angle sensor arranged to detect a momentary pitching angle of the tip blade part relative to the main blade part.
  • a suitable sensor or detector could be arranged in or on the tip blade section to determine the momentary position of the tip blade part relative to a reference position such as a default or furled position. This sensor can be connected to a control unit as described above, for controlling the compressed-air source.
  • the rotor blade according to the invention preferably comprises a safety mechanism realised to pitch the rotor tip blade part out of the wind (i.e. to "furl" the rotor blade) under certain circumstances.
  • a safety mechanism could also be actuated deliberately or automatically in the event of a fault in the rotor blade pitching system.
  • the safety mechanism can cause the rotating part of the fluid bearing - and therefore also the tip blade part - to return to a default or initial position.
  • the compressed-air source can stop the flow of pressurized air into the bearing, and any air in the bearing can be allowed to vacate the bearing.
  • the bearing returns to its default position, and the tip blade part returns to its default position also.
  • any interruption of the pressurized air into the bearing will simply result in the tip blade section returning to its default position, so that the safety mechanism in this case is automatic.
  • a default position might be a "resting" position of the bearing in which the bearing pads are essentially in contact with each other and are not separated by an air cushion.
  • the rotor blade according to the invention preferably comprises a fluid duct or air duct for connecting the inlet to the compressed-air source.
  • the air duct is arranged in the main blade part to extend from the compressed air source, which can be arranged in the hub or in the nacelle, to the fluid bearing, which can be arranged in the tip blade part.
  • such a duct can be incorporated inside the body of a blade part during or after the manufacture of a composite blade with an essentially hollow body section.
  • the rotor blade comprises a stationary or fixed pivot rod arranged to extend at least partially into the tip blade part, and wherein the tip blade part is arranged to rotate about the pivot rod.
  • the pivot rod can be made of any robust material, for example steel.
  • the pivot rod can extend into the main blade part so that the main blade part and the tip blade part are connected in a colinear fashion.
  • the fluid bearing can comprise an essentially cylindrical shape, with the pivot rod extending through the centre of the fluid bearing, and the bearing pads can each comprise a disc shape with a circular opening to accommodate the pivot rod.
  • the bearing can be realised to comprise a sleeve extending through its centre, dimensioned to fit closely about the pivot rod to minimize any play.
  • the pivot rod can be mounted onto only the outer bearing pad, and the bearing pads can each comprise an uninterrupted circular disc shape.
  • the bearing preferably comprises an air-tight seal so that essentially no air escapes from between the bearing pads.
  • a movement of a moveable bearing part results in a rotation of the tip blade part.
  • an outward radial motion of the moveable bearing part is preferably translated into a rotational motion of the tip blade section.
  • Such a motion translation can be achieved in a number of ways.
  • a protruding pin arranged to travel along a helically arranged groove can translate a radial direction of motion of the moveable bearing part into a rotation of the tip blade section about its axis of rotation. This can take effect within the bearing itself.
  • a surface of the bearing can comprise a helical groove in the manner of a threaded groove
  • the moveable bearing pad can comprise a pin arranged to move along this groove, thus compelling the moveable bearing pad to rotate.
  • the motion translation preferably allows any useful pitching angle to be achieved.
  • a pin and helical groove for motion translation can be realised to permit a pitching angle between 0° (furled position) and a maximum pitching position during normal operation, for example a few degrees, and an "extreme" or brake/stop angle of about 90°.
  • the motion translation preferably comprises an infinite "resolution", so that any pitching angle or fraction of a pitching angle is obtainable over the allowable range.
  • a pivot rod could assist the motion of the moveable part of the bearing.
  • a pin or helical groove of a motion translation means can be formed on the pivot, while the complementary part (groove or pin) of the motion translation means can be formed on a corresponding part of the moveable bearing pad.
  • a rotor blade of a wind turbine generally includes some kind of lightning protection system to provide a path to ground in the event of a lightning strike.
  • a lightning protection system can comprise a metal conductor arranged along the outside of the rotor blade to the hub, where it is connected to a further conductor leading to ground.
  • a preferred arrangement involves arranging the metal conductor inside the blade itself. Therefore, in a further preferred embodiment of the invention, if a pivot rod is used, it is incorporated into a lightning protection system of the rotor blade.
  • the tip blade part is releasably connected to the main blade part, so that the tip section can relatively easily be disconnected or dismounted from the main blade part and for repair or replacement by another tip section.
  • the blade sections can be realised to comprise some kind of connecting means such as a flange connection, a bolted connection, a threaded connection, etc.
  • the connecting means is realised to maintain an essentially smooth surface contour over the blade outer surface.
  • the connecting means is realised to be accessible from the outside, so that a maintenance worker can conveniently dismount the tip section from the main blade section as required.
  • a rotor blade is preferably essentially smooth over its entire surface, so that the aerodynamic properties of the blade are not compromised. Therefore, in a further preferred embodiment of the invention, the rotor blade comprises an essentially circular cross-sectional shape at a joint between the main blade part and the tip blade part. When the pitching angle is altered, the tip section rotates about the main blade section essentially without any interruption in a surface contour.
  • the rotor speed of the rotor can be regulated efficiently by adjusting the pitching angle of a tip blade section of the two-part blade according to the invention.
  • the main blade part can be shaped with only a minor airfoil shape, and can be pitched to a lesser extent than a prior art rotor blade.
  • the main blade section is mounted in a stationary manner to the hub, i.e. the main blade part is not rotatable about an axis of rotation, and there is no pitch bearing between the main blade part and the hub. In such an embodiment, only the tip blade part of the split blade is pitched. This simplifies the design of the main blade part considerably.
  • the main blade part comprises a uniform cross-section essentially over its entire length, between the point at which it is mounted to the hub and a point approaching a joint or interface at which the main blade part is connected to the tip blade part.
  • the main blade part can have a circular cross-section, or preferably an elliptical or tear-drop cross-section for improved aerodynamic performance.
  • Such an elliptical or tear-drop cross-section can transition smoothly into a circular cross-section at the point of connection to the tip blade part.
  • the two-part blade comprises a coupling means for coupling a hoisting apparatus to a blade part of the rotor blade.
  • the tip section is preferably releasably mounted to the main blade section, the tip section could relatively easily be detached from the blade when this is "parked" in a downward position, and lowered to the ground or to a ship in the case of an offshore wind turbine.
  • the coupling means could comprise brackets or hooks arranged in the body of the main blade section and the tip section.
  • a bracket can be set into the body of a blade section and covered, as long as it is not required, by a removable cover set into the blade surface.
  • a maintenance worker can rappel from the hub down to the tip section, attach a cable or rope to the main blade section and also to the tip section, and can then disconnect the tip section from the main blade section.
  • a block-and-tackle arrangement or other hoisting means can then be used to lower the tip section to ground, and the tip section is essentially suspended from the main blade section during the lowering manoeuvre.
  • a new or replacement tip section can be mounted to the main blade section in the same way, by lifting it into place where it can be mounted onto the main blade section.
  • Fig. 1 shows a prior art rotor blade 5 mounted to a hub 20 of a wind turbine.
  • the hub 20 rotates when wind is captured by the rotor blade 5, causing a rotor to rotate so that generator (not shown) located in a nacelle 21 can output electrical energy accordingly.
  • the blade 5 comprises a pronounced airfoil section 50 over a considerable part of its length.
  • it is connected to the hub 20 by means of a circular pitch bearing 51 driven by a motor (not shown).
  • a centrifugal force acts on the blade outer end in the direction F shown.
  • such a prior art blade is expensive to manufacture.
  • a long blade is correspondingly heavy and requires a powerful pitch motor and a large pitch bearing.
  • the mass and cost increase essentially according to the square-cube law.
  • Fig. 2 shows a two-part rotor blade 1 and a rotor blade pitching system according to a first embodiment of the invention.
  • the rotor blade 1 comprises a long main blade part 11 with a uniform cross-section over most or all of its length, and a tip blade part 10 with an airfoil section shaped to allow wind energy to be extracted from the wind.
  • the main blade part 11 is mounted in a fixed manner to the hub 20, without any pitch bearing.
  • a connecting interface 21, for example a simple flange 21, can be arranged in or on the hub 20 to match the cross-sectional shape of the main blade part 11, which can be, for example, elliptical or tear-shaped.
  • An interface between the main blade part 11 and the tip blade part 10 can be circular in cross-section.
  • the tip blade part 10 is rotatably mounted to the main blade part 11 by means of a bearing 30 and a pivot rod 31.
  • the bearing 30 is a fluid bearing with a stationary bearing pad 302 and a moveable bearing pad 301.
  • the pivot rod 31 is embedded in the body of the tip blade part 10.
  • a compressed air source 32 arranged in the hub 20 can force compressed air via an air duct 33 through an inlet 34 formed in the outer bearing pad 301 and into a space between bearing pads 301, 302 of the bearing 30 to form an air cushion 340.
  • the compressed air is forced into the bearing 30 in a direction opposite to the direction F of the centrifugal force acting on the tip blade part 10.
  • the bearing 30 and/or pivot rod is realised such that a motion of the outer bearing pad 301 in a radially outward direction D is translated into a rotation R A of the pivot rod 31 and therefore also of the tip blade part 10 relative to the main blade part 11 about an axis of rotation A. With relatively little effort, therefore, the tip blade section 10 can be pitched at a desired angle into or out of the wind, as the need arises.
  • the compressed air source 32 can be connected to such a bearing in each of the rotor blades (usually but not necessarily three) of a wind turbine.
  • Fig. 3 shows a wind turbine 2 according to an embodiment of the invention.
  • three rotor blades 1 are connected to the hub 20 to turn a rotor of a generator located in the nacelle 21, which is mounted on a tower 23.
  • a sensor 35 for example a strain gauge 35 or other suitable sensor 35, mounted on a two-part blade 1, can detect a wind strength.
  • An output of this sensor 35 can be processed by a processor 36 to determine a momentary desired pitching angle.
  • the desired pitching angle is communicated to a compressed air source 32 in the hub 20 by means of a wireless signal 37.
  • Fig. 4 shows a maintenance procedure being carried out on a two-part rotor blade 1 of a wind turbine 2 according to a further embodiment of the invention.
  • a maintenance vessel 7 has been directed to an offshore wind turbine.
  • a maintenance technician has deployed from an opening in the hub 20 to the lower or outer end of a downward-pointing two-part rotor blade 1.
  • a cable 70 has been connected to a tip blade part 10 and to a winch 70 of the maintenance vessel 7 over a cable attachment means 110 on the main blade part 11.
  • the maintenance technician has released the tip blade part 10 from the main blade part 11 so that the tip blade part 10 can be lowered to the vessel 7.
  • a replacement tip blade part can be lifted into place for connection to the main blade part 11.

Claims (14)

  1. Rotorblattanstellanordnung für ein zweiteiliges Rotorblatt (1) einer Windturbine (2) mit
    - einem Fluidlager (30), das so ausgelegt ist, dass es einen Blattspitzenteil (10) des zweiteiligen Windturbinenrotorblatts (1) so mit einem Blatthauptteil (11) des zweiteiligen Windturbinenrotorblatts (1) verbindet, dass der Blattspitzenteil (10) in Bezug auf den Blatthauptteil (11) um eine Rotationsachse (A) drehbar ist, und
    - einem Anstellwinkelverstellmittel (32) zum Erzielen eines bestimmten Anstellwinkels des Blattspitzenteils (10) zwecks Erhöhen und Verringern einer Drehzahl eines Rotors der Windturbine (2).
  2. Rotorblattanstellanordnung nach Anspruch 1, bei der das Anstellwinkelverstellmittel (32) eine Fluidquelle (32) umfasst, die ein geregeltes Volumen an Druckfluid in das Fluidlager (30) einspeist, so dass sich der Blattspitzenteil (10) in Bezug zum Blatthauptteil (11) dreht, wobei ein Fluidvolumen in einem direkten Verhältnis zu einem Anstellwinkel des Blattspitzenteils (10) in Bezug zum Blatthauptteil (11) steht.
  3. Rotorblattanstellanordnung nach Anspruch 2, bei der das Anstellwinkelverstellmittel (32) so ausgelegt ist, dass es das Fluid in einer Richtung in das Fluidlager (30) einspeist, die der Richtung einer Zentrifugalkraft (F), die bei einer Drehung des zweiteiligen Blatts (1) auf den Blattspitzenteil (10) einwirkt, im Wesentlichen entgegengesetzt ist.
  4. Rotorblattanstellanordnung nach Anspruch 2 oder 3, bei der die Fluidquelle (32) eine Druckluftquelle umfasst.
  5. Rotorblattanstellanordnung nach einem der Ansprüche 2 bis 4, die eine Steuereinheit (36) umfasst, welche die Fluidquelle (32) auf der Grundlage eines Sensorausgangssignals (37) so steuert, dass ein Sollanstellwinkel erzielt wird.
  6. Zweiteiliges Windturbinenrotorblatt (1) mit einem Blattspitzenteil (10), einem Blatthauptteil (11) und einem Fluidlager (30), das so ausgelegt ist, dass es den Blattspitzenteil (10) so mit dem Blatthauptteil (11) verbindet, dass der Blattspitzenteil (10) in Bezug auf den Blatthauptteil (11) um eine Rotationsachse (A) drehbar ist, wobei das Fluidlager (30) für die Verbindung mit einem Anstellwinkelverstellmittel (32) zum Erzielen eines bestimmten Anstellwinkels des Blattspitzenteils (10) zwecks Erhöhen und Verringern einer Drehzahl eines Rotors der Windturbine (2) ausgelegt ist.
  7. Zweiteiliges Rotorblatt nach Anspruch 6, bei dem das Fluidlager (30) einen Einlass (34) zum Einspeisen eines Druckfluids (340) aus einer Fluidquelle (32) in einer Richtung (D) in das Fluidlager (30) umfasst, die der Richtung einer Zentrifugalkraft (F), die bei einer Drehung des zweiteiligen Blatts (1) auf den Blattspitzenteil (10) einwirkt, im Wesentlichen entgegengesetzt ist.
  8. Zweiteiliges Rotorblatt nach Anspruch 7, das eine Fluidleitung (33) zum Verbinden des Fluideinlasses (34) mit der Druckfluidquelle (32) umfasst, wobei die Fluidleitung (33) so angeordnet ist, dass sie von einem unteren Ende des Blatthauptteils (11) aus durch einen Körper des Blatthauptteils (11) zum Einlass (43) des Fluidlagers (30) verläuft.
  9. Zweiteiliges Rotorblatt nach einem der Ansprüche 6 bis 8, bei dem der Blattspitzenteil (10) so angeordnet ist, dass er sich um eine Schwenkachse (31) dreht, die so angeordnet ist, dass sie zumindest teilweise in den Blattspitzenteil (10) hinein verläuft.
  10. Zweiteiliges Rotorblatt nach Anspruch 9, bei dem die Schwenkachse (31) in ein Blitzschutzsystem des Rotorblatts (1) integriert ist.
  11. Zweiteiliges Rotorblatt nach einem der Ansprüche 6 bis 10, bei dem der Blatthauptteil (11) zwischen einem inneren Ende und einem äußeren Ende einen im Wesentlichen gleichförmigen Querschnitt umfasst.
  12. Zweiteiliges Rotorblatt nach einem der Ansprüche 6 bis 11, bei dem eine Verbindungsstelle (12) zwischen dem Blatthauptteil (11) und dem Blattspitzenteil (10) einen im Wesentlichen runden Querschnitt umfasst.
  13. Windturbine (2) mit einer Anzahl zweiteiliger Windturbinenrotorblätter (1) nach einem der Ansprüche 6 bis 12, die so angeordnet sind, dass sie einen Rotor der Windturbine (2) drehen, wobei die Drehzahl des Rotors gemäß einem Anstellwinkel eines Blattspitzenteils (10) eines zweiteiligen Rotorblatts (1) erhöht und verringert und der Anstellwinkel eines Blattspitzenteils (10) eines zweiteiligen Rotorblatts (1) durch eine Rotorblattanstellanordnung nach einem der Ansprüche 1 bis 5 geregelt wird.
  14. Verfahren zum Verstellen eines Anstellwinkels eines zweiteiligen Windturbinenrotorblatts (1) einer Windturbine (2) nach Anspruch 13, das folgende Schritte umfasst:
    - Bestimmen eines Sollanstellwinkels für den Blattspitzenteil (10) eines zweiteiligen Rotorblatts (1),
    - Bestimmen eines Ausmaßes an Bewegung eines beweglichen Lagerteils (301) des Fluidlagers (30) des zweiteiligen Blatts (1) zum Erzielen dieses Anstellwinkels und
    - entsprechendes Steuern eines Anstellwinkelverstellmittels (32) der Rotorblattanstellanordnung, so dass der bewegliche Lagerteil (301) des Fluidlagers (30) um dieses Ausmaß in Bewegung versetzt wird.
EP12158855.2A 2012-03-09 2012-03-09 Anordnung zum Verstellen des Anstellwinkels eines Rotorblatts Not-in-force EP2636890B1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP12158855.2A EP2636890B1 (de) 2012-03-09 2012-03-09 Anordnung zum Verstellen des Anstellwinkels eines Rotorblatts
DK12158855.2T DK2636890T3 (en) 2012-03-09 2012-03-09 Rotorvingepitchinganordning
US13/783,709 US20130236307A1 (en) 2012-03-09 2013-03-04 Rotor blade pitching arrangement

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Application Number Priority Date Filing Date Title
EP12158855.2A EP2636890B1 (de) 2012-03-09 2012-03-09 Anordnung zum Verstellen des Anstellwinkels eines Rotorblatts

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US20130236307A1 (en) 2013-09-12
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